Numerical Evaluation of an Ejector-Enhanced Resonant Pulse Combustor with a Poppet Inlet Valve and a Converging Exhaust Nozzle
52nd AIAA/SAE/ASEE Joint Propulsion Conference
2016-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2016
|Engineering Index Backfile | 1929
|SAE Technical Papers | 1929
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